Effect of Rotor- and Stator-blade Modifications on Surge Performance of an 11-stage Axial-flow Compressor II - Redesigned Compressor for XJ-40-WE-6 Engine
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Conrad, E William↗
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Results for “AXIAL FLOW COMPRESSOR”
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Experimental Investigation of an Axial-flow Compressor Inlet Stage Operating at Transonic Relative Inlet Mach Numbers III : Blade-row Performance of Stage with Transonic Rotor and Subsonic Stator at Corrected Tip Speeds of 800 and 1000 Feet Per Secon
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Schwenk, Francis C↗
An Investigation of Continuous Boundary-layer Removal in an Axial Flow Compressor with Porous Walls
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Wlodarski, John↗
Investigation of an Axial-flow Compressor Rotor Having NACA High-speed Blade Sections (a(sub 2)i(sub 8b) Series) at Mean Radius Relative Inlet Mach Numbers up to 1.13
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Savage, Melvyn↗
Analysis of Performance of Four Symmetrical-diagram-type Subsonic Inlet-stage Axial-flow Compressors
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Jackson, Robert J↗
Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections I : design, over-all performance and stall characteristics
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Schwenk, Francis C↗
Review of high-performance axial-flow-compressor blade-element theory
This report presents a review of current compressor blade-element theory with particular emphasis on application to the transonic high-performance compressor. A discussion of the significant parameters of total-pressure loss and deviation angle is presented, and an indication of the extent of available knowledge and the problems involved in the determination of blade-element characteristics is given. Some recent results and considerations in this pursuit and suggestions for further avenues of investigation are indicated.
Lieblein, Seymour↗
Analysis of part-speed operation for high-pressure-ratio multistage axial-flow compressors
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Benser, William A↗
Experimental Investigation of a 0.4 Hub-tip Diameter Ratio Axial-flow Compressor Inlet Stage at Transonic Inlet Relative Mach Numbers I : Rotor Design and Over-all Performance at Tip Speeds from 60 to 100 Percent of Design
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Serovy, George K↗
Experimental Investigation of Rotating Stall and Blade Vibration in the Axial-flow Compressor of a Turbojet Engine
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Huppert, Merle C↗
Investigation of Three Highly Loaded Subsonic-inlet-stage Axial-flow Compressors Employing Varying Radial Gradients of Energy Addition
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Standahar, Raymond M↗
Effect of Inlet-air Baffles on Rotating-stall and Stress Characteristics of an Axial-flow Compressor in a Turbojet Engine
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Huntley, S C↗
Experimental investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers II : stage and blade-element performance
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Montgomery, John C↗
Axial-flow Compressor Rotating-stall and Rotor-blade Vibration Survey
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Calvert, Howard F↗
Investigation of a High-performance Axial-flow Compressor Transonic Inlet Rotor Designed for 37.5 Pounds Per Second Per Square Foot of Frontal Area : Aerodynamic Design and Overall Performance
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Savage, Melvyn↗
Effect of annular inlet baffles on rotating stall, blade vibration, and performance of an axial flow compressor in a turbojet engine
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Johnson, Donald F↗
Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections III : comparison of blade-element performance with three levels of solidity
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Schwenk, Francis C↗
Effect of inlet temperature on rotating stall and blade vibrations in a multistage axial-flow compressor
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Medeiros, Arthur A↗